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专利名称：Vertically integrated stringers发明人：Moselage III, John H.申请号：AU2013251284申请日：20131104公开号：AU2013251284A1公开日：20140612
摘要：#$%^&*AU2013251284A120140612.pdf##### VERTICALLY INTEGRATEDSTRINGERS ABSTRACT Apparatus and methods provide for the reinforcement of variouscomponents of an aircraft (100) utilizing vertically-oriented circumferential stringers.According to embodiments described herein, barrel skin of an aircraft fuselage (102) maybe reinforced using stringers (112) that are vertically-oriented and circumferential.According to additional embodiments, the wing stringers (114, 116) of a wing (108a, 108b)can be aligned with circumferential stringers (112). According to further embodiments,the wing (508) may also have one or more wing spars (610a, 610b, 612a, 612b) having anelliptical aperture (614a, 614b, 616a, 616b). The shape of the elliptical aperture may beconfigured for attachment to a fuselage (102) so that an outer surface of the aperture isdisposed proximate to an inner surface of the fuselage (102). 1/9 >( CDC C-1
申请人：The Boeing Company
代理人：Spruson & Ferguson
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